▸Orbital parameters

Orbit class	SSO
Inclination	97.4483°
Eccentricity	0.0002776
Period	94.7 min
Apogee	507 km
Perigee	504 km
Mean motion	15.20124434 rev/day
RAAN	145.7218°
Arg of perigee	121.2167°
Mean anomaly	238.9340°
B*	3.7586e-4
Rev at epoch	1,487

▸Two-line element set (TLE)

EPOCH Jul 6, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 68420U 26067E 26187.44384272 .00008060 00000-0 37586-3 0 9995

2 68420 97.4483 145.7218 0002776 121.2167 238.9340 15.20124434 14872

▸ source OMM (JSON)

{
  "OBJECT_NAME": "ERMIS-2",
  "OBJECT_ID": "2026-067E",
  "EPOCH": "2026-07-06T10:39:08.011+00:00",
  "MEAN_MOTION": 15.20124434,
  "ECCENTRICITY": 0.0002776,
  "INCLINATION": 97.4483,
  "RA_OF_ASC_NODE": 145.7218,
  "ARG_OF_PERICENTER": 121.2167,
  "MEAN_ANOMALY": 238.934,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 68420,
  "REV_AT_EPOCH": 1487,
  "BSTAR": 0.00037586,
  "MEAN_MOTION_DOT": 0.0000806,
  "MEAN_MOTION_DDOT": 0
}

Reconstructed from CelesTrak OMM mean-elements (element-set number is a placeholder). TLE/OMM data is approximate. Not for operational use or collision avoidance.

▸Satellite metadata

Name	ERMIS-2
Operator	University of AthensHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Greece
Launch date	Mar 30, 2026HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	10HIGHvia GCAT — Jonathan McDowell's General Catalog
Mission purpose	—
Object class	PAYLOADHIGH

▸Data quality

Score85 / 100

Claims7

Sources1

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org

▸Actions

GET /api/v1/satellites/68420

//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.